View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 14781U 84021B 23156.46717157 .00001357 00000-0 16559-3 0 9996
2 14781 97.6567 133.8525 0006767 234.0985 125.9603 14.84868500 92402
| Epoch (UTC): | 05 June 2023 11:12:43 |
| Eccentricity: | 0.0006767 |
| inclination: | 97.6567° |
| perigee height: | 609 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 133.8525° |
| argument of perigee: | 234.0985° |
| revolutions per day: | 14.84868500 |
| mean anomaly at epoch: | 125.9603° |
| orbit number at epoch: | 9240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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